Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment
Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Pradyumna, S. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2010 |
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| Schlagwörter: |
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| Anmerkung: |
© Springer-Verlag 2010 |
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| Übergeordnetes Werk: |
Enthalten in: Acta mechanica - Springer Vienna, 1965, 218(2010), 3-4 vom: 25. Dez., Seite 295-308 |
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volume:218 ; year:2010 ; number:3-4 ; day:25 ; month:12 ; pages:295-308 |
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| DOI / URN: |
10.1007/s00707-010-0424-4 |
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OLC2030134899 |
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| 520 | |a Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. | ||
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10.1007/s00707-010-0424-4 doi (DE-627)OLC2030134899 (DE-He213)s00707-010-0424-4-p DE-627 ger DE-627 rakwb eng 530 VZ Pradyumna, S. verfasserin aut Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2010 Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. Cylindrical Shell Dynamic Stability Spherical Shell Piezoelectric Layer Laminate Composite Plate Gupta, Abhishek aut Enthalten in Acta mechanica Springer Vienna, 1965 218(2010), 3-4 vom: 25. Dez., Seite 295-308 (DE-627)129511676 (DE-600)210328-X (DE-576)014919141 0001-5970 nnns volume:218 year:2010 number:3-4 day:25 month:12 pages:295-308 https://doi.org/10.1007/s00707-010-0424-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_21 GBV_ILN_22 GBV_ILN_59 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2020 GBV_ILN_4700 AR 218 2010 3-4 25 12 295-308 |
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10.1007/s00707-010-0424-4 doi (DE-627)OLC2030134899 (DE-He213)s00707-010-0424-4-p DE-627 ger DE-627 rakwb eng 530 VZ Pradyumna, S. verfasserin aut Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2010 Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. Cylindrical Shell Dynamic Stability Spherical Shell Piezoelectric Layer Laminate Composite Plate Gupta, Abhishek aut Enthalten in Acta mechanica Springer Vienna, 1965 218(2010), 3-4 vom: 25. Dez., Seite 295-308 (DE-627)129511676 (DE-600)210328-X (DE-576)014919141 0001-5970 nnns volume:218 year:2010 number:3-4 day:25 month:12 pages:295-308 https://doi.org/10.1007/s00707-010-0424-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_21 GBV_ILN_22 GBV_ILN_59 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2020 GBV_ILN_4700 AR 218 2010 3-4 25 12 295-308 |
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10.1007/s00707-010-0424-4 doi (DE-627)OLC2030134899 (DE-He213)s00707-010-0424-4-p DE-627 ger DE-627 rakwb eng 530 VZ Pradyumna, S. verfasserin aut Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2010 Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. Cylindrical Shell Dynamic Stability Spherical Shell Piezoelectric Layer Laminate Composite Plate Gupta, Abhishek aut Enthalten in Acta mechanica Springer Vienna, 1965 218(2010), 3-4 vom: 25. Dez., Seite 295-308 (DE-627)129511676 (DE-600)210328-X (DE-576)014919141 0001-5970 nnns volume:218 year:2010 number:3-4 day:25 month:12 pages:295-308 https://doi.org/10.1007/s00707-010-0424-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_21 GBV_ILN_22 GBV_ILN_59 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2020 GBV_ILN_4700 AR 218 2010 3-4 25 12 295-308 |
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10.1007/s00707-010-0424-4 doi (DE-627)OLC2030134899 (DE-He213)s00707-010-0424-4-p DE-627 ger DE-627 rakwb eng 530 VZ Pradyumna, S. verfasserin aut Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2010 Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. Cylindrical Shell Dynamic Stability Spherical Shell Piezoelectric Layer Laminate Composite Plate Gupta, Abhishek aut Enthalten in Acta mechanica Springer Vienna, 1965 218(2010), 3-4 vom: 25. Dez., Seite 295-308 (DE-627)129511676 (DE-600)210328-X (DE-576)014919141 0001-5970 nnns volume:218 year:2010 number:3-4 day:25 month:12 pages:295-308 https://doi.org/10.1007/s00707-010-0424-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_21 GBV_ILN_22 GBV_ILN_59 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2020 GBV_ILN_4700 AR 218 2010 3-4 25 12 295-308 |
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10.1007/s00707-010-0424-4 doi (DE-627)OLC2030134899 (DE-He213)s00707-010-0424-4-p DE-627 ger DE-627 rakwb eng 530 VZ Pradyumna, S. verfasserin aut Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2010 Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. Cylindrical Shell Dynamic Stability Spherical Shell Piezoelectric Layer Laminate Composite Plate Gupta, Abhishek aut Enthalten in Acta mechanica Springer Vienna, 1965 218(2010), 3-4 vom: 25. Dez., Seite 295-308 (DE-627)129511676 (DE-600)210328-X (DE-576)014919141 0001-5970 nnns volume:218 year:2010 number:3-4 day:25 month:12 pages:295-308 https://doi.org/10.1007/s00707-010-0424-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_21 GBV_ILN_22 GBV_ILN_59 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2020 GBV_ILN_4700 AR 218 2010 3-4 25 12 295-308 |
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Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment |
| abstract |
Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. © Springer-Verlag 2010 |
| abstractGer |
Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. © Springer-Verlag 2010 |
| abstract_unstemmed |
Abstract This paper reports the nonlinear dynamic stability characteristics of laminated composite cylindrical (CYL) and spherical (SPH) shells integrated with piezoelectric layers using the finite element method. The shells are subjected to a thermal environment in addition to the in-plane periodic load and the electric load. The theoretical formulation considers Sanders’ approximation for doubly curved shells, and von Kármán type nonlinear strains are incorporated into the first-order shear deformation theory (FSDT). The formulation includes the effects of transverse shear, in-plane and rotatory inertia. The in-plane periodic load is taken as the parametric excitation in the governing equation. The nonlinear matrix amplitude equation is obtained by employing Galerkin’s method. The correctness of the formulation is established by comparing the authors’ results with those available in the published literature. Detailed parametric studies are carried out to investigate the effects of different parameters on the dynamic stability characteristics of laminated composite shells. © Springer-Verlag 2010 |
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Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment |
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